TM 1-1520-240-MTF
2-85
IN-FLIGHT (CONT.)
(5) Accomplish Power Recovery prior to
1000’ AGL.
(a)
Load Rotor by relaxing pressure on
Thrust Control Lever allowing it to
come up as required if RRPM is
above 100%.
(b)
FADEC NR% rheostat — 100%
position.
(c)
Reestablish 100% RRPM, safe
airspeed, and altitude.
(d)
Climb back to altitude where PA
was noted and record following:
1 Free Air Temperature.
2 Fuel Quantity.
(e)
Record previously noted: RRPM.
PA,
Pedal
Separation,
and
Unusual Vibrations (as applicable).
(6) Compare data to chart in Section V for
proper RRPM. Ensure conversion from
PA and FAT to DA.
13. 712 Engine TEAC check, if required. (Refer to
Section IV.)
14. 714A Power Assurance Check, if required.
(Refer to Section IV.)
15. Fuel consumption check — STOP.
16. Navigation and Communication. (Refer to
Section IV.)
17. Miscellaneous (as required).
a. Vertical velocity indicators
b. Turn and slip indicators.
